HAM-STD HS1-430 AIRFOIL (hs1430-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: HAM-STD HS1-430 AIRFOIL (hs1430-il) Reynolds number: 500,000 Max Cl/Cd: 27.41 at α=9.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-hs1430-il-500000.txt Download as CSV file: xf-hs1430-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: HAM-STD HS1-430 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1689 0.07106 0.06546 -0.1054 0.9888 0.1171
-19.500 -1.1764 0.06791 0.06222 -0.1052 0.9872 0.1183
-19.250 -1.1805 0.06487 0.05907 -0.1054 0.9858 0.1194
-19.000 -1.1821 0.06199 0.05605 -0.1058 0.9844 0.1204
-18.750 -1.1766 0.05987 0.05396 -0.1060 0.9832 0.1219
-18.500 -1.1698 0.05773 0.05181 -0.1066 0.9820 0.1232
-18.250 -1.1612 0.05551 0.04956 -0.1075 0.9808 0.1244
-18.000 -1.1502 0.05346 0.04746 -0.1086 0.9798 0.1258
-17.750 -1.1389 0.05148 0.04540 -0.1096 0.9789 0.1272
-17.500 -1.1271 0.04961 0.04344 -0.1105 0.9781 0.1286
-17.250 -1.1102 0.04765 0.04137 -0.1124 0.9773 0.1298
-17.000 -1.0893 0.04592 0.03966 -0.1144 0.9765 0.1316
-16.750 -1.0647 0.04431 0.03805 -0.1169 0.9758 0.1332
-16.500 -1.0682 0.04303 0.03675 -0.1136 0.9708 0.1343
-16.250 -1.0515 0.04163 0.03530 -0.1142 0.9684 0.1358
-16.000 -1.0324 0.04027 0.03389 -0.1151 0.9669 0.1373
-15.750 -1.0127 0.03892 0.03246 -0.1162 0.9656 0.1388
-15.500 -0.9905 0.03763 0.03107 -0.1176 0.9645 0.1401
-15.250 -0.9663 0.03639 0.02988 -0.1191 0.9638 0.1420
-15.000 -0.9412 0.03522 0.02871 -0.1208 0.9631 0.1436
-14.750 -0.9136 0.03412 0.02758 -0.1228 0.9625 0.1454
-14.500 -0.8858 0.03302 0.02644 -0.1248 0.9620 0.1472
-14.250 -0.8965 0.03255 0.02593 -0.1185 0.9550 0.1482
-14.000 -0.8764 0.03166 0.02496 -0.1187 0.9534 0.1496
-13.750 -0.8519 0.03073 0.02397 -0.1197 0.9523 0.1511
-13.500 -0.8242 0.02979 0.02309 -0.1211 0.9515 0.1532
-13.250 -0.7964 0.02888 0.02218 -0.1225 0.9507 0.1550
-13.000 -0.7703 0.02803 0.02132 -0.1235 0.9498 0.1569
-12.750 -0.7431 0.02722 0.02048 -0.1246 0.9489 0.1587
-12.500 -0.7406 0.02687 0.02009 -0.1204 0.9435 0.1600
-12.250 -0.7211 0.02623 0.01937 -0.1198 0.9409 0.1614
-12.000 -0.6934 0.02541 0.01858 -0.1207 0.9393 0.1636
-11.750 -0.6672 0.02466 0.01787 -0.1213 0.9379 0.1657
-11.500 -0.6404 0.02398 0.01720 -0.1220 0.9366 0.1676
-11.250 -0.6338 0.02366 0.01688 -0.1184 0.9307 0.1690
-11.000 -0.6126 0.02313 0.01632 -0.1177 0.9276 0.1709
-10.750 -0.5863 0.02257 0.01571 -0.1181 0.9255 0.1727
-10.500 -0.5656 0.02206 0.01520 -0.1172 0.9219 0.1745
-10.250 -0.5457 0.02154 0.01472 -0.1162 0.9177 0.1764
-10.000 -0.5177 0.02097 0.01415 -0.1168 0.9148 0.1782
-9.750 -0.5032 0.02069 0.01386 -0.1144 0.9075 0.1799
-9.500 -0.4897 0.02043 0.01359 -0.1118 0.8995 0.1816
-9.250 -0.4836 0.02026 0.01338 -0.1076 0.8886 0.1831
-9.000 -0.4571 0.01984 0.01290 -0.1076 0.8812 0.1849
-8.750 -0.4345 0.01941 0.01246 -0.1069 0.8709 0.1867
-8.500 -0.4086 0.01899 0.01204 -0.1068 0.8590 0.1884
-8.250 -0.3799 0.01861 0.01161 -0.1073 0.8439 0.1904
-8.000 -0.3512 0.01828 0.01118 -0.1078 0.8253 0.1925
-7.750 -0.3264 0.01807 0.01082 -0.1074 0.8023 0.1946
-7.500 -0.3068 0.01797 0.01055 -0.1058 0.7802 0.1964
-7.250 -0.2908 0.01792 0.01036 -0.1034 0.7639 0.1977
-7.000 -0.2725 0.01776 0.01011 -0.1017 0.7495 0.1995
-6.750 -0.2551 0.01754 0.00989 -0.0997 0.7386 0.2017
-6.500 -0.2410 0.01745 0.00976 -0.0970 0.7276 0.2035
-6.250 -0.2258 0.01739 0.00966 -0.0945 0.7172 0.2053
-6.000 -0.2096 0.01735 0.00957 -0.0921 0.7040 0.2073
-5.750 -0.1944 0.01735 0.00948 -0.0895 0.6905 0.2093
-5.500 -0.1787 0.01734 0.00940 -0.0870 0.6770 0.2111
-5.250 -0.1640 0.01737 0.00933 -0.0843 0.6648 0.2125
-5.000 -0.1489 0.01717 0.00912 -0.0817 0.6520 0.2150
-4.750 -0.1420 0.01708 0.00900 -0.0773 0.6398 0.2174
-4.500 -0.1305 0.01701 0.00893 -0.0739 0.6275 0.2195
-4.250 -0.1229 0.01706 0.00891 -0.0696 0.6126 0.2215
-4.000 -0.1146 0.01714 0.00891 -0.0655 0.5909 0.2235
-3.750 -0.1048 0.01727 0.00893 -0.0617 0.5659 0.2255
-3.500 -0.1016 0.01759 0.00905 -0.0566 0.5254 0.2272
-3.250 -0.1026 0.01814 0.00930 -0.0507 0.4694 0.2285
-3.000 -0.0982 0.01864 0.00953 -0.0461 0.4184 0.2300
-2.750 -0.1021 0.01931 0.00984 -0.0400 0.3325 0.2328
-2.500 -0.0914 0.01964 0.01001 -0.0369 0.2962 0.2356
-2.250 -0.0741 0.01979 0.01012 -0.0349 0.2831 0.2383
-2.000 -0.0551 0.01994 0.01023 -0.0334 0.2755 0.2409
-1.750 -0.0348 0.02006 0.01032 -0.0320 0.2707 0.2433
-1.500 -0.0139 0.02020 0.01042 -0.0308 0.2672 0.2455
-1.250 0.0069 0.02035 0.01054 -0.0296 0.2645 0.2473
-1.000 0.0283 0.02049 0.01065 -0.0285 0.2627 0.2489
-0.750 0.0487 0.02049 0.01067 -0.0273 0.2614 0.2528
-0.500 0.0698 0.02055 0.01076 -0.0262 0.2602 0.2561
-0.250 0.0912 0.02066 0.01089 -0.0252 0.2591 0.2589
0.000 0.1124 0.02080 0.01103 -0.0241 0.2581 0.2615
0.250 0.1336 0.02097 0.01120 -0.0231 0.2571 0.2642
0.500 0.1549 0.02116 0.01138 -0.0221 0.2561 0.2666
0.750 0.1761 0.02137 0.01158 -0.0211 0.2552 0.2687
1.000 0.1971 0.02161 0.01180 -0.0200 0.2543 0.2703
1.250 0.2177 0.02179 0.01200 -0.0190 0.2536 0.2744
1.500 0.2382 0.02199 0.01223 -0.0179 0.2530 0.2790
1.750 0.2583 0.02223 0.01250 -0.0168 0.2524 0.2835
2.000 0.2788 0.02248 0.01278 -0.0158 0.2518 0.2886
2.250 0.2999 0.02275 0.01306 -0.0149 0.2514 0.2942
2.500 0.3210 0.02294 0.01333 -0.0141 0.2511 0.3063
2.750 0.3418 0.02313 0.01362 -0.0132 0.2507 0.3251
3.000 0.3616 0.02310 0.01391 -0.0123 0.2504 0.3902
3.250 0.3777 0.02265 0.01424 -0.0107 0.2501 0.5721
3.500 0.3961 0.02270 0.01469 -0.0093 0.2498 0.6650
3.750 0.4166 0.02296 0.01511 -0.0084 0.2494 0.7072
4.000 0.4375 0.02324 0.01553 -0.0075 0.2491 0.7406
4.250 0.4579 0.02352 0.01600 -0.0064 0.2487 0.7778
4.500 0.4764 0.02385 0.01663 -0.0048 0.2484 0.8377
4.750 0.4953 0.02441 0.01738 -0.0031 0.2481 0.8946
5.000 0.5154 0.02502 0.01803 -0.0018 0.2477 0.9232
5.250 0.5370 0.02564 0.01868 -0.0010 0.2474 0.9395
5.500 0.5577 0.02627 0.01931 -0.0001 0.2470 0.9525
5.750 0.5842 0.02702 0.02005 -0.0005 0.2466 0.9625
6.000 0.6092 0.02773 0.02074 -0.0005 0.2462 0.9709
6.250 0.6471 0.02856 0.02156 -0.0036 0.2457 0.9745
6.500 0.6862 0.02942 0.02240 -0.0069 0.2452 0.9773
6.750 0.7228 0.03027 0.02323 -0.0097 0.2444 0.9805
7.000 0.7556 0.03112 0.02405 -0.0118 0.2436 0.9842
7.250 0.7828 0.03192 0.02483 -0.0126 0.2430 0.9880
7.500 0.8169 0.03265 0.02554 -0.0150 0.2424 0.9891
7.750 0.8511 0.03339 0.02625 -0.0175 0.2418 0.9905
8.000 0.8871 0.03416 0.02698 -0.0203 0.2411 0.9921
8.250 0.9219 0.03486 0.02766 -0.0229 0.2405 0.9939
8.500 0.9534 0.03556 0.02835 -0.0248 0.2399 0.9956
8.750 0.9834 0.03634 0.02916 -0.0265 0.2391 0.9974
9.000 1.0139 0.03717 0.03000 -0.0284 0.2383 0.9991
9.250 1.0380 0.03787 0.03072 -0.0289 0.2375 1.0000
9.500 1.0490 0.03832 0.03117 -0.0268 0.2368 1.0000
9.750 1.0600 0.03880 0.03167 -0.0247 0.2362 1.0000
10.000 1.0704 0.03933 0.03220 -0.0226 0.2354 1.0000
10.250 1.0818 0.03982 0.03269 -0.0206 0.2347 1.0000
10.500 1.0939 0.04031 0.03318 -0.0187 0.2340 1.0000
10.750 1.1057 0.04082 0.03369 -0.0169 0.2333 1.0000
11.000 1.1176 0.04135 0.03421 -0.0151 0.2326 1.0000
11.250 1.1304 0.04184 0.03469 -0.0134 0.2319 1.0000
11.500 1.1448 0.04226 0.03509 -0.0120 0.2312 1.0000
11.750 1.1623 0.04254 0.03532 -0.0109 0.2303 1.0000
12.000 1.1742 0.04313 0.03595 -0.0093 0.2296 1.0000
12.250 1.1832 0.04393 0.03679 -0.0074 0.2286 1.0000
12.500 1.1936 0.04468 0.03758 -0.0057 0.2277 1.0000
12.750 1.2054 0.04539 0.03831 -0.0042 0.2267 1.0000
13.000 1.2181 0.04608 0.03902 -0.0029 0.2256 1.0000
13.250 1.2313 0.04678 0.03973 -0.0018 0.2246 1.0000
13.500 1.2449 0.04750 0.04044 -0.0007 0.2236 1.0000
13.750 1.2605 0.04813 0.04105 0.0001 0.2226 1.0000
14.000 1.2808 0.04846 0.04132 0.0004 0.2215 1.0000
14.250 1.2945 0.04936 0.04226 0.0013 0.2204 1.0000
14.500 1.3062 0.05048 0.04344 0.0021 0.2192 1.0000
14.750 1.3187 0.05159 0.04459 0.0028 0.2179 1.0000
15.000 1.3323 0.05264 0.04566 0.0033 0.2165 1.0000
15.250 1.3487 0.05348 0.04648 0.0036 0.2152 1.0000
15.500 1.3697 0.05394 0.04688 0.0036 0.2139 1.0000
15.750 1.3903 0.05445 0.04736 0.0036 0.2126 1.0000
16.000 1.3973 0.05616 0.04918 0.0044 0.2112 1.0000
16.250 1.4081 0.05757 0.05064 0.0048 0.2096 1.0000
16.500 1.4223 0.05870 0.05177 0.0051 0.2081 1.0000
16.750 1.4423 0.05928 0.05231 0.0049 0.2068 1.0000
17.000 1.4709 0.05907 0.05200 0.0043 0.2054 1.0000
17.250 1.4666 0.06191 0.05502 0.0055 0.2039 1.0000
17.500 1.4719 0.06392 0.05711 0.0060 0.2022 1.0000
17.750 1.4824 0.06544 0.05867 0.0062 0.2007 1.0000
18.000 1.4989 0.06638 0.05959 0.0061 0.1995 1.0000
18.250 1.5188 0.06696 0.06013 0.0059 0.1983 1.0000
18.500 1.5080 0.07071 0.06411 0.0068 0.1964 1.0000
18.750 1.5088 0.07336 0.06688 0.0071 0.1945 1.0000
19.000 1.5155 0.07542 0.06899 0.0071 0.1930 1.0000
19.250 1.5242 0.07727 0.07086 0.0069 0.1918 1.0000
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